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    Analysis of Multiple Fatigue Cracks—Part I: Theory

    Source: Journal of Tribology:;1992:;volume( 114 ):;issue: 003::page 455
    Author:
    M. C. Dubourg
    ,
    B. Villechaise
    DOI: 10.1115/1.2920905
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper analyzes the effects of multiple cracks situated in the contact zone vicinity of an elastic isotropic component, modeled as a half-plane. Friction between the crack faces is taken into account using Coulomb’s law. Straight arbitrarily oriented cracks are considered. Any contact condition can be modeled between the crack faces as well as any loading condition over the half-plane surface, including complete loading cycles. The method has been tested for up to 5 cracks and shows no limitation in crack number. Further, the method is general as no prior assumptions concerning the state of the crack, i.e., the slip-stick-open configurations along the crack are required. The stress intensity factors (SIFs) calculated for two crack configuration are compared with those obtained for single cracks.
    keyword(s): Friction , Coulomb's law , Stress , Fracture (Materials) , Cycles AND Fatigue cracks ,
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      Analysis of Multiple Fatigue Cracks—Part I: Theory

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/110915
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    contributor authorM. C. Dubourg
    contributor authorB. Villechaise
    date accessioned2017-05-08T23:39:40Z
    date available2017-05-08T23:39:40Z
    date copyrightJuly, 1992
    date issued1992
    identifier issn0742-4787
    identifier otherJOTRE9-28497#455_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110915
    description abstractThis paper analyzes the effects of multiple cracks situated in the contact zone vicinity of an elastic isotropic component, modeled as a half-plane. Friction between the crack faces is taken into account using Coulomb’s law. Straight arbitrarily oriented cracks are considered. Any contact condition can be modeled between the crack faces as well as any loading condition over the half-plane surface, including complete loading cycles. The method has been tested for up to 5 cracks and shows no limitation in crack number. Further, the method is general as no prior assumptions concerning the state of the crack, i.e., the slip-stick-open configurations along the crack are required. The stress intensity factors (SIFs) calculated for two crack configuration are compared with those obtained for single cracks.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAnalysis of Multiple Fatigue Cracks—Part I: Theory
    typeJournal Paper
    journal volume114
    journal issue3
    journal titleJournal of Tribology
    identifier doi10.1115/1.2920905
    journal fristpage455
    journal lastpage461
    identifier eissn1528-8897
    keywordsFriction
    keywordsCoulomb's law
    keywordsStress
    keywordsFracture (Materials)
    keywordsCycles AND Fatigue cracks
    treeJournal of Tribology:;1992:;volume( 114 ):;issue: 003
    contenttypeFulltext
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